EP0436533B1 - Corps en nid d'abeille, ayant notamment des toles en s partiellement renforcees - Google Patents

Corps en nid d'abeille, ayant notamment des toles en s partiellement renforcees Download PDF

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Publication number
EP0436533B1
EP0436533B1 EP89900246A EP89900246A EP0436533B1 EP 0436533 B1 EP0436533 B1 EP 0436533B1 EP 89900246 A EP89900246 A EP 89900246A EP 89900246 A EP89900246 A EP 89900246A EP 0436533 B1 EP0436533 B1 EP 0436533B1
Authority
EP
European Patent Office
Prior art keywords
layers
sheet metal
stack
honeycomb body
body according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP89900246A
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German (de)
English (en)
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EP0436533A1 (fr
Inventor
Wolfgang Maus
Helmut Swars
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vitesco Technologies Lohmar Verwaltungs GmbH
Original Assignee
Emitec Gesellschaft fuer Emissionstechnologie mbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Emitec Gesellschaft fuer Emissionstechnologie mbH filed Critical Emitec Gesellschaft fuer Emissionstechnologie mbH
Publication of EP0436533A1 publication Critical patent/EP0436533A1/fr
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Publication of EP0436533B1 publication Critical patent/EP0436533B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
    • F01N3/28—Construction of catalytic reactors
    • F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
    • F01N3/2807—Metal other than sintered metal
    • F01N3/281—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
    • B01J35/56—
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2330/00—Structure of catalyst support or particle filter
    • F01N2330/02—Metallic plates or honeycombs, e.g. superposed or rolled-up corrugated or otherwise deformed sheet metal
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/1234—Honeycomb, or with grain orientation or elongated elements in defined angular relationship in respective components [e.g., parallel, inter- secting, etc.]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/1241—Nonplanar uniform thickness or nonlinear uniform diameter [e.g., L-shape]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness

Definitions

  • the present invention relates to a metallic honeycomb body, in particular a catalyst carrier body for internal combustion engines, according to the preamble of claim 1.
  • honeycomb bodies are known from EP-A-0 245 737. Structured sheets intertwined in opposite directions can be used to fill many different cross-sectional shapes, resulting in bodies that are very resistant to thermal alternating loads.
  • the typical shape of the sheets, which resembles an S, is relatively elastic and makes it possible to connect all of the sheets at their ends with a casing tube, which has considerable mechanical advantages over spirally wound honeycomb bodies.
  • catalyst carrier bodies consisting of smooth and corrugated sheet metal strips that the sheet metal strips can have different thicknesses. How this can be used to improve the attachment of the body to a casing tube is not apparent from this document.
  • the object of the present invention is to create a honeycomb body, in particular a catalyst carrier body, which has a fastening on the jacket tube that is more resistant to tearing.
  • a honeycomb body with the characterizing features of claim 1 is proposed.
  • the stack of mutually intertwined, at least partially structured metal sheets on its upper side and / or its lower side and / or in its interior has individual layers of greater thickness, either by using thicker metal sheets or by having several thin metal sheets of the same structure close together.
  • the effect of these thicker layers of sheet metal is that, owing to their greater mechanical strength, they cannot be easily torn off on the tubular casing.
  • these thicker layers can also hold on to the sheet metal layers adjacent to them, so that they either do not tear off on the casing tube, or at least are held in place despite the tear-off due to the thick layer. If the individual sheet metal layers of the stack are soldered to one another, preferably on one or both end faces, the thicker layers conduct the tensile forces which arise in the outer region in the vicinity of the casing tube into the interior of the honeycomb body, so that the forces are distributed over considerably more connection points , which significantly increases the lifespan of the body.
  • the middle sheet metal layer of the stack should have a greater thickness than the other layers. This is not a problem in terms of production technology, in particular since the greater thickness is achieved by stacking many thin sheets together.
  • the reinforcement of the middle sheet layer leads to a symmetrical structure of the resulting body, which is also advantageous for the distribution of forces.
  • the proposed embodiment according to claim 4 offers particular advantages. Since oval or elliptical shapes are sensitive to deformations with changing internal pressure, an approximately S-shaped connecting bridge between the straight or weakly rounded regions of the casing tube is a measure which is particularly advantageous for the stability of this shape. Here, too, individual thicker layers distribute the forces occurring outside in the vicinity of the casing tube much better evenly into the interior of the catalyst carrier body, which u. a. also the noise development is reduced.
  • the thicker sheet layers should be smooth sheet layers. While many different sheet metal structures are known from the prior art for forming channels which are permeable to exhaust gas, the most frequently used type of structure is an alternating layering of smooth and corrugated sheet metal layers. In this case, it makes sense to reinforce some of the smooth sheet metal layers. Smooth sheet metal layers deform less than corrugated sheet metal under tension and can therefore transmit the occurring forces better than corrugated sheet metal sheets.
  • the thicker sheet layers should not extend over the entire width of the stack, ie not over the entire axial length of the honeycomb body, but can consist of one or more strips lying one behind the other in the axial direction.
  • an end-face high-temperature soldering is also used for these special honeycomb bodies, which preferably extends to a depth of a few millimeters.
  • Figure 1 shows a stack of alternately layered smooth 1 and corrugated 2 sheets, as it is suitable for producing a honeycomb body according to the invention.
  • the stack 3 has a length L, a height H and a width B.
  • the width B corresponds to the later axial expansion of the honeycomb body
  • the product of length and height corresponds to the later cross-sectional area of the finished honeycomb body.
  • Such a stack 3 can be devoured in opposite directions around two fixed points 5 and 6, as is already known from the prior art.
  • the lateral ends 4 of the individual sheet metal layers can be connected in whole or in part with a casing tube, in particular by high-temperature soldering.
  • the sheet metal layers 1, 2 are also soldered to one another at high temperatures in the finished honeycomb body, in particular in the region of the end faces.
  • some of the sheet layers are thicker than the rest of the stack 3.
  • the top sheet metal layer 8, the bottom sheet metal layer 9 and the middle sheet metal layer 10 are thicker, either by using thicker sheets or by stacking several smooth sheets on top of one another.
  • These thicker sheet metal layers can extend all or in part over the entire width B of the stack, but they can also, as indicated in the present case, only be formed as strips 8a, 8b or 9a, 9b or 10a, 10b, which are extend only over part b of the width B of the stack.
  • FIG. 2 shows a honeycomb body as it arises after the stack from FIG. 1 has been devoured in opposite directions.
  • the intertwined sheet metal layers 1, 2 are arranged in a jacket tube 7 and at least in some areas connected to it by joining technology, in particular high-temperature soldering.
  • the thicker sheet metal layers 8, 9, 10, which are also connected to the casing tube 7, can transmit forces from the outer region to the interior in this form of honeycomb bodies.
  • these thicker sheet layers 8, 9, 10 do not tear off easily from the casing tube 7 and thereby stabilize the neighboring layers.
  • the original top and bottom layers of the stack are bent around the fixed points 5 and 6 in the finished honeycomb body and thus have a double thickness.
  • the thicker sheet metal layers 8, 9, 10 do not need to extend over the entire axial extent of the honeycomb body, indicated by the arrow.
  • the thicker sheet layers 8, 9, 10 can consist, for example, of two partial strips 9a, 9b and 10a, 10b of width b arranged on the end face. It is important that the partial strips are connected to the casing tube 7 by joining technology and preferably also have connections to their neighboring layers. It is particularly favorable if the sheet metal layers 1, 2, 8, 9, 10 are soldered to each other a few millimeters deep on the end face.
  • FIG. 3 A further exemplary embodiment, for which the application of the present invention is particularly suitable, is shown in FIG. 3. It is a honeycomb body with an elliptical cross section.
  • the individual structured sheet metal layers are only indicated by dashed lines. Some of the sheet layers, namely the top 38, bottom 39 and middle 40 layers of the original stack from which this body is made, are thicker than the other layers. Due to their firm connection to the casing tube 37, they stabilize the entire body and also prevent deformation of the casing tube 37 due to high internal pressure within certain limits.
  • Such an elliptical honeycomb body like many other shapes, can also be produced from a stack of structured metal sheets by intertwining the ends in opposite directions around the fixed points 35, 36. Only the location of the fixed points and the shape of the starting stack are different than in the production of honeycomb bodies with a round cross-section.
  • a honeycomb body with a so-called oval cross section is shown in FIG.
  • Such bodies can also be produced by intertwining a stack of structured sheets 1, 2 around fixed points 45, 46.
  • the top 48, bottom 49 and middle 50 layers are reinforced.
  • the present invention is particularly suitable for catalyst support bodies with an oval or elliptical cross section, which are to be used as the main catalyst in motor vehicles.
  • Typical sheet thicknesses are z. B. for the non-reinforced sheets 0.03 - 0.05 mm and for the reinforced sheets 0.15 - 2.0 mm.

Abstract

Un corps en nid d'abeille, notamment un support de catalyseur, qui présente de préférence une section transversale circulaire, ovale ou elliptique, se compose d'une pile de tôles structurées (1, 2) entrelacées en sens inverse et agencées dans une enveloppe tubulaire (7). Afin de stabiliser l'ensemble du corps et d'empêcher les tôles (1, 2) de se détacher de l'enveloppe tubulaire (7), certaines tôles (8, 9, 10) sont plus épaisses que les autres, étant composées d'une feuille métallique plus épaisse ou d'une pluralité de fines tôles étroitement liées les unes aux autres. Les tôles plus épaisses stabilisent l'ensemble du corps et empêchent l'enveloppe tubulaire de se déformer sous une pression interne et une température élevées, même lorsque celle-ci présente une section transversale ovale ou elliptique.

Claims (8)

  1. Corps alvéolaire, en particulier corps support pour catalyseur, de préférence à section ronde, ovale ou elliptique, contenant dans une enveloppe tubulaire un empilement vrillé tête-bêche de tôles au moins partiellement structurées, celles-ci étant reliées à l'enveloppe de façon matériellement jointive au moins dans des parties de zones, caractérisé en ce qu'une ou plusieurs (8, 9, 10 ; 38, 39, 40 ; 48, 49, 50) des couches de tôles (1, 2) de l'empilement (3) présentent, sur toute ou partie de la longueur (L) et/ou de la largeur (B) de l'empilement, une épaisseur supérieure à celle des autres couches, cette (ces) couche(s) (8, 9, 10 ; 38, 39, 40 ; 48, 49, 50) étant formée(s) par une tôle plus épaisse ou par une pluralité de tôles plus minces identiquement structurées et disposées attenantes les unes aux autres.
  2. Le corps alvéolaire de la revendication 1, caractérisé en ce que la couche de tôle (10 ; 40 ; 50) située approximativement au milieu de l'empilement (3) présente une épaisseur supérieure à celle des autres couches.
  3. Le corps alvéolaire de la revendication 1 ou 2, caractérisé en ce que la couche de tôle supérieure (8 ; 38 ; 48) et/ou la couche de tôle inférieure (9 ; 39 ; 49) de l'empilement (3) présentent une épaisseur supérieure.
  4. Le corps alvéolaire de la revendication 1 ou 2, caractérisé en ce que, dans le cas des formes ovales ou, respectivement, elliptiques, la (les) couche(s) de tôle (40 ; 50) d'épaisseur supérieure forme(nt) un (des) pont(s) de liaison en forme approximative de S entre les zones planes ou, respectivement, à faible courbure du corps support de catalyseur, pont(s) qui conduit (conduisent) l'énergie produite de l'extérieur dans l'intérieur du corps support de catalyseur.
  5. Le corps alvéolaire de l'une des revendications 1, 2, 3 ou 4, caractérisé en ce que la (les) couche(s) de tôle(s) d'épaisseur supérieure (8, 9, 10 ; 38, 39, 40 ; 48, 49, 50) sont des couches de tôles lisses.
  6. Le corps alvéolaire de l'une des revendications précédentes, caractérisé en ce que les couches de tôles plus épaisses (8, 9, 10 ; 38, 39, 40 ; 48, 49, 50) ne s'étendent pas sur toute la longueur axiale du corps support de catalyseur, mais sont formées par une ou plusieurs bandes (10a, 10b) s'étendant l'une derrière l'autre en direction axiale.
  7. Le corps alvéolaire de la revendication 6, caractérisé en ce qu'il n'est prévu de bande (10a, 10b) qu'à une extrémité frontale ou qu'aux deux extrémités frontales, sur une largeur (b) de 1 à 3 cm en direction axiale.
  8. Le corps alvéolaire de l'une des revendications précédentes, caractérisé en ce que le corps support de catalyseur est, frontalement, totalement ou partiellement soudé à haute température, de préférence sur une profondeur de 3 à 10 millimètres.
EP89900246A 1988-02-11 1988-12-19 Corps en nid d'abeille, ayant notamment des toles en s partiellement renforcees Expired - Lifetime EP0436533B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE8801788U DE8801788U1 (fr) 1988-02-11 1988-02-11
DE8801788U 1988-02-11

Publications (2)

Publication Number Publication Date
EP0436533A1 EP0436533A1 (fr) 1991-07-17
EP0436533B1 true EP0436533B1 (fr) 1993-06-23

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EP89900246A Expired - Lifetime EP0436533B1 (fr) 1988-02-11 1988-12-19 Corps en nid d'abeille, ayant notamment des toles en s partiellement renforcees

Country Status (8)

Country Link
US (1) US5102743A (fr)
EP (1) EP0436533B1 (fr)
JP (1) JPH03502544A (fr)
BR (1) BR8807886A (fr)
DE (2) DE8801788U1 (fr)
MX (1) MX171154B (fr)
RU (1) RU1838640C (fr)
WO (1) WO1989007488A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7108168B2 (en) 2002-01-03 2006-09-19 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb structure and method for applying adhesive and brazing material to the structure
DE102009035612A1 (de) 2009-07-31 2011-02-03 Emitec Gesellschaft Für Emissionstechnologie Mbh Wabenkörper und Verfahren zu seiner Herstellung

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992002714A1 (fr) * 1990-07-30 1992-02-20 Emitec Gesellschaft Für Emissionstechnologie Mbh Corps en nid d'abeilles a chauffage electrique, notamment corps de support de catalyseur, a structures internes de support
DE4024942A1 (de) * 1990-08-06 1992-02-13 Emitec Emissionstechnologie Monolithischer metallischer wabenkoerper mit variierender kanalzahl
DE4025434A1 (de) * 1990-08-10 1992-02-13 Emitec Emissionstechnologie Wabenkoerper mit querschnittsbereichen unterschiedlicher kanalgroessen, insbesondere katalysator-traegerkoerper
DE4105469A1 (de) * 1991-02-21 1992-09-03 Emitec Emissionstechnologie Wabenkoerper mit schraubensinn
US5170624A (en) * 1991-04-05 1992-12-15 W. R. Grace & Co.-Conn. Composite catalytic converter
US5240682A (en) * 1991-05-06 1993-08-31 W. R. Grace & Co.-Conn Reinforced corrugated thin metal foil strip useful in a catalytic converter core, a catalytic converter core containing said strip and an electrically heatable catalytic converter containing said core
JP2509478B2 (ja) * 1991-05-09 1996-06-19 昭和飛行機工業株式会社 ハニカム構造体およびその製造方法
US6288008B1 (en) * 1991-07-04 2001-09-11 Matsumoto Kokan Co., Ltd. Metallic catalyst support and production method thereof
DE4129893A1 (de) * 1991-09-09 1993-03-11 Emitec Emissionstechnologie Anordnung zur temperaturmessung und/oder heizung und deren verwendung in einem wabenkoerper, insbesondere katalysator-traegerkoerper
BR9206958A (pt) * 1991-12-21 1995-11-28 Emitec Emissionstechnologie Corpo de colmeia com uma estrutura interna que é segura por uma moldura
BR9306740A (pt) * 1992-07-14 1998-12-08 Emitec Emissionstechnologie Corpo de colmeia metálico de camadas de chapas entrelaçadas e processo para sua fabricação
EP0590171B1 (fr) * 1992-09-26 1996-12-04 Showa Aircraft Industry Co., Ltd. Structure en nid d'abeilles pour la purification de gaz d'échappement et son procédé de fabrication
US5866230A (en) * 1993-01-11 1999-02-02 Emitec Gesellschaft Fuer Emissionstechnologie Gmbh Extruded honeycomb body of ceramic and/or metallic material with increased flexibility
US5422083A (en) * 1993-06-29 1995-06-06 W. R. Grace & Co.-Conn. Reinforced converter body
DE4411302C1 (de) * 1994-03-31 1995-10-19 Degussa Verfahren zur Herstellung eines beschichteten, monolithischen Trägerkatalysators
DE4418630A1 (de) * 1994-05-27 1995-11-30 Emitec Emissionstechnologie Wabenkörper auf Blechlagen unterschiedlicher Vormaterialien
JPH0824670A (ja) * 1994-07-11 1996-01-30 Usui Internatl Ind Co Ltd 排気ガス浄化用メタルハニカム体
DE19507299A1 (de) * 1995-03-02 1996-09-05 Emitec Emissionstechnologie Wabenkörper mit nur teilweiser Anbindung an ein Mantelrohr
US5846495A (en) * 1995-07-12 1998-12-08 Engelhard Corporation Structure for converter body
DE19530835A1 (de) * 1995-08-22 1997-02-27 Emitec Emissionstechnologie Verfahren zum Herstellen eines Wabenkörpers unter Verwendung schichtartig aufgebauter Bleche mit Lotmaterial
DE19530871A1 (de) * 1995-08-22 1997-02-27 Emitec Emissionstechnologie Verfahren zum Herstellen eines gelöteten Wabenkörpers unter Verwendung schichtartig aufgebauter Bleche
DE19530850A1 (de) * 1995-08-22 1997-02-27 Emitec Emissionstechnologie Verfahren zum Herstellen eines Wabenkörpers aus zumindest zum Teil schichtartig aufgebauten Metallblechlagen
DE19530853A1 (de) * 1995-08-22 1997-02-27 Emitec Emissionstechnologie Verfahren zum Herstellen eines Wabenkörpers aus zwei unterschiedlich aufgebauten Metallblecharten
US6036926A (en) * 1995-10-20 2000-03-14 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb body of sheet metal layers with reinforcing structures and catalytic reactor having the honeycomb body
DE19704144A1 (de) * 1997-02-04 1998-08-06 Emitec Emissionstechnologie Extrudierter Wabenkörper, insbesondere Katalysator-Trägerkörper, mit verstärkter Wandstruktur
DE19704129A1 (de) * 1997-02-04 1998-08-06 Emitec Emissionstechnologie Wabenkörper, insbesondere Katalysator-Trägerkörper,mit verstärkter Wandstruktur
US6136450A (en) * 1997-02-04 2000-10-24 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb body, in particular a catalytic converter carrier body, with a reinforced wall structure
DE19844075A1 (de) * 1998-09-25 2000-03-30 Man Nutzfahrzeuge Ag Kompakter Kreuzkanalmischer
DE19908834A1 (de) * 1999-03-01 2000-09-07 Emitec Emissionstechnologie Katalysatoranordnung mit Katalysator-Trägerkörpern und Vorrichtung sowie Verfahren zu deren Herstellung
DE19922358C1 (de) * 1999-05-14 2001-01-25 Helmut Swars Wabenkörper
DE19946462A1 (de) * 1999-09-28 2001-03-29 Bayerische Motoren Werke Ag Katalysator-Trägerkörper mit gestapelten und/oder gewickelten Blechlagen
DE10011286B4 (de) * 2000-03-08 2007-08-02 Emitec Gesellschaft Für Emissionstechnologie Mbh Verwendung eines Lötmaterials zum Verlöten von Metallblechen
DE10329002A1 (de) * 2003-06-27 2005-01-20 Emitec Gesellschaft Für Emissionstechnologie Mbh Aufbau einer metallischen Wabenstruktur und Verfahren zu dessen Herstellung
DE102005028044A1 (de) * 2005-06-17 2006-12-28 Emitec Gesellschaft Für Emissionstechnologie Mbh Herstellung von, insbesondere großen, Wabenkörpern für die mobile Abgasnachbehandlung
US20070131481A1 (en) * 2005-12-12 2007-06-14 John Mordarski Method and apparatus for attenuating sound in a vehicle exhaust system
DE102012004918A1 (de) 2012-03-09 2013-09-12 Emitec Gesellschaft Für Emissionstechnologie Mbh Wabenkörper zur Abgasnachbehandlung

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2902779C2 (de) * 1979-01-25 1985-09-26 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co. KG, 7000 Stuttgart Matrix für einen katalytischen Reaktor zur Abgasreinigung bei Brennkraftmaschinen
DE3333941A1 (de) * 1983-09-20 1985-04-04 Karl Kässbohrer Fahrzeugwerke GmbH, 7900 Ulm Fraese
DE8528096U1 (de) * 1985-10-02 1985-11-14 Karl Kässbohrer Fahrzeugwerke GmbH, 7900 Ulm Schneefräse
DE3760479D1 (en) * 1986-05-12 1989-09-28 Interatom Honeycomb body, particularly a catalyst carrier, provided with opposedly folded metal sheet layers, and its manufacturing process

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7108168B2 (en) 2002-01-03 2006-09-19 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb structure and method for applying adhesive and brazing material to the structure
US7562805B2 (en) 2002-01-03 2009-07-21 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb structure and method for applying adhesive and brazing material to the structure
DE102009035612A1 (de) 2009-07-31 2011-02-03 Emitec Gesellschaft Für Emissionstechnologie Mbh Wabenkörper und Verfahren zu seiner Herstellung

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MX171154B (es) 1993-10-05
WO1989007488A1 (fr) 1989-08-24
BR8807886A (pt) 1990-11-13
DE3882054D1 (de) 1993-07-29
EP0436533A1 (fr) 1991-07-17
JPH03502544A (ja) 1991-06-13
US5102743A (en) 1992-04-07
RU1838640C (ru) 1993-08-30
DE8801788U1 (fr) 1989-06-15
JPH0471580B2 (fr) 1992-11-16

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